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48-04-02: Wing Rib Rework

FAA order 48-04-02 is an airworthiness directive. The FAA's subject line: Wing Rib Rework. It names American Champion Aircraft 7 Citabria and Champ: about 429 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
American Champion Aircraft Corp.
Models
11AC, 11BC, 7AC
On this site
American Champion Aircraft 7 Citabria and Champ 429 registered

Dates and paperwork

Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,660 characters)
48-04-02 AERONCA: Applies to 7AC Serial Numbers 7AC-1 Through 7AC-7129; 11BC Serial Numbers 11BC-1 Through 11BC-173; and 11AC Serial Numbers 11AC-1 and Up. \n\n\tCompliance required by March 1, 1948. \n\n\tInspect the wing leading edge for buckled nose ribs or loose PK screws by pressing leading edge skin with hand to nose ribs. If the skin can be depressed beyond the normal wing contour, other than the extreme nose radius, indicated by section A-A in Figure 1, the fabric should be cut open on the bottom surface just forward of the front spar for thorough inspection. Item No. 1 below should be accomplished on all wings whether damage has occurred or not, whereas item No. 2 pertains only to damaged ribs found in the above inspection. Repair need not be made if buckling is confined to area forward of section A-A of Figure 1. \n\n\n\n\t1.\tTo help prevent further failures of the nose ribs five additional No. 4 x 1/4 PK screws or, as an alternate, Cherry CR163-4-2 rivets or equivalentare to be installed in all nose ribs. Four PK screws or rivets are to be installed on the top surface and one PK screw or rivet is to be installed in the bottom as shown in Figure 1. Apply dope liberally under the PK screw head before tightening. It is not necessary to remove the fabric to accomplish this modification. \n\n\t2.\tDamaged ribs should be cut away at the top and bottom of spar. The new nose ribs are installed by means of two gussets on the side of the ribs as shown in Figure 1. Factory kits, Aeronca P/N 5-185-2 and 5-190-2, are to be used. \n\n\t(Aeronca Helps and Hints No. 17 with three supplements thereto covers this same subject.)

Related safety bulletins advice on the same designs, not orders

2018-07-12CE-18-20 · Electrical Power
2013-07-12CE-13-40 · Flight Compartment
2011-07-06CE-11-43 · Flight Controls
2010-07-23CE-10-39 · Equipment - Furnishings
2009-03-20CE-09-20 · Equipment - Furnishings

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/48-04-02.json · aircraft systems.